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    中低雷诺数可压缩冲击射流的流动与传热特性

    Flow and Heat Transfer Characteristics of Compressible Impinging Jets at Low to Moderate Reynolds Numbers

    • 摘要: 采用大涡模拟方法研究马赫数(Ma)为0.784、冲击高度(H/D)为5、雷诺数(Re)为3300~8000的可压缩冲击射流的流动和传热特性。模拟得到了冲击射流的平均速度和温度,以及旋涡的演化过程,揭示了传热随着雷诺数的增加而增强的趋势。在Re=8000时,初级涡提前破碎为小尺度涡且未发现合并的旋涡。对冲击射流的温度和压力进行动态模态分解(DMD),并特别关注展向和撞击板处的相干结构。结果表明,当斯特劳哈尔数(St)为0.56时,DMD模态所识别的相干结构呈大尺度的对称结构,当St=1.04时,对称结构向下游移动并逐渐分化为小尺度结构,这也表明大尺度的初级涡经过撞击后形成尺度更小的二次涡。

       

      Abstract: Large eddy simulation (LES) is used to study the flow and heat transfer characteristics of compressible impinging jets with a Mach number (Ma) of 0.784, an impact height (H/D) of 5, and a Reynolds number (Re) ranging from 3300 to 8000. The average velocity and temperature, as well as the evolution process of vortices, are obtained. It is revealed that the heat transfer increases with the increase in Re. At a Re of 8000, the primary vortices break into small-scale vortices in advance, with no merged vortices found in the simulation results. In addition, dynamic mode decomposition (DMD) is performed for the temperature and pressure of the impinging jets, particularly focusing on the coherent structure at the spanwise location and on the impact plate. The results show that at a frequency St of 0.56, the coherent structures identified by DMD modes are large-scale symmetric structures. At frequency St of 1.04, these symmetric structures move downstream and gradually differentiate into small-scale structures. This indicates that the large-scale primary vortex forms a smaller scale secondary vortex upon impacting.

       

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